View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 06324U 72104B 23151.91530487 .00000276 00000-0 88582-4 0 9998
2 06324 74.0791 34.8589 0009291 327.8342 32.2247 14.43932486649106
Epoch (UTC): | 31 May 2023 21:58:02 |
Eccentricity: | 0.0009291 |
inclination: | 74.0791° |
perigee height: | 739 km |
apogee height: | 752 km |
right ascension of ascending node: | 34.8589° |
argument of perigee: | 327.8342° |
revolutions per day: | 14.43932486 |
mean anomaly at epoch: | 32.2247° |
orbit number at epoch: | 64910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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